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Page 1
FAA Flammability Certification of Electrical and Electronic Components
Kendall D. HesterJames M. Peterson
Boeing Commercial Airplanes Group
International Aircraft Fire and Cabin Safety Research ConferenceOctober 22-25, 2001
Page 2
Boeing Goals• Comply with Regulatory Requirements • Continuously Improve Safety of Flight• Utilize Supplementary Internal and Industry
Standards • Improve procurement cost of equipment
– Utilize industry data – Use engineering skills and experience– Work together with our suppliers– Eliminate unnecessary and non-value added processes
and testing
Page 3
Typical Elements of Electronic Equipment
• Electric Wire• Printed Wiring Boards (PWBs)• Cathode Ray Tubes• Liquid Crystal Displays • Transformers• Switches• Small Components (Diodes, Resistors, etc.)
Page 6
History of Electronic Equipment Usage in Commercial Transport Airplanes
• In the early years, electronic equipment consisted primarily of simple avionics in the flight deck and E/E bay
• Later, additional electronic units and sensors were added all over the airplane
• In recent years, there has been a great expansion of in-flight passenger entertainment systems, up to Internet access on seat-powered laptop computers
Page 7
Electronic Equipment Design Criteria
• Military specifications used to control the fire properties of electronic equipment.
• Many of these military specifications have been recently canceled.– Example older requirement - Printed Wiring
Board material shall be epoxy/glass (Type GF) or other material with equivalent or better temperature, arc, and flame resistance, in accordance with MIL-P-13949.
Page 8
FAA Flammability Requirements
• FAA regulations were changed in 1967, and new flammability requirements and test methods were added– New standards for side-walls, ceilings, etc.
• Small parts did not have to be tested – Except for small parts (such as …… small
electrical parts) that would not contribute significantly to the propagation of a fire…
• Electronic components were viewed as “small parts”
Page 9
FAA Flammability Requirements (cont)
• In the 1960’s, there were only a few electronic components in the EE bay and flight deck. – Only materials compliant to the Military Standards
(self-extinguishing) were used• Today significantly more electrical/electronic
components are used• Military production standards have been
canceled and replaced by industry production standards
Page 10
FAA Flammability Requirements (cont)
• Aerospace industry standards require either– IPC 4101 flammability test be done on laminates
making up a PWB before board is assembled or– UL 94 V0 test on the finished PWB– No industry requirement for 12-sec vertical
• FAA clarified that regulatory testing of electronic components requires
– FAR tests - 12-sec vertical Bunsen burner test (e.g., printed wiring boards, PWBs)
– or approved alternatives
Page 11
FAA Flammability Requirements (cont)
• Aerospace PWBs built to industry standards always pass FAA test with high margin
• FAA receptive to “equivalent safety finding” to approve PWBs meeting industry standards without requiring FAR 12-sec vertical test
• FAR 21, § 21.21(b)(1)– …. any airworthiness provisions not complied with
are compensated for by factors that provide an equivalent level of safety …
Page 12
Equivalent Safety Finding
• Plan for establishing equivalent safety finding– Analysis of IPC, UL, and FAR test procedures– Analysis of the sample testing by suppliers
(i.e. the on-going process control)– Test a representative sample of IPC and UL compliant
PWB materials using the FAR 12-sec vertical test• Bare printed wiring board laminates• Complete multilayer printed wiring boards• Printed wiring assemblies with conformal coat
Page 13
FAA Flammability Requirements (cont)
• When an “equivalent safety finding” is granted, PWBswill be FAA-approved by process control
• Showing compliance by process control is a significant need for electronics – Electronics are in constant redesign
• Testing by part number is inefficient and extremely expensive in the long run
– Continuous process control provides better assurance • As opposed the current one time test
– Most electronics redesign does not change materials• Re-layout of PWBs and microcircuits• Software updates
Page 14
Reasons for Electronic Redesign
• Airline requests for increased functionality– More features and options – In-flight entertainment
• Product improvements– Updates, problem resolution, production
improvements• Component obsolescence
– Cancellation of the military specifications– Commercial components have a shorter production
life due to high volume users
Page 15
PWBs are the Most Frequently Changed Item
Typical Materials Redesign ImpactsSmall electrical components:
Microcircuits, resistors,capacitors, switches, etc.
Frequently changebut small are parts
Flexi-cables, small wire cables Seldom changeDisplays Seldom changeGaskets Seldom changeConnectors Seldom changeSheet metal, screws, etc. No impact on the
flammability analysisPrinted wiring boards Frequently change
Page 16
Process Control Methods
• Boeing is incorporating process control methods for design and manufacturing – DO-178 (Example of Software process control) – DO-254 (Example of hardware process control) – ISO-9000 (Example of quality by process control) – AS-9000 (Example of quality by process control)
• Process control provides– Improved quality, reliability, and performance– Lower costs– Shorter design cycle times
Page 17
Use of Industry Standards
Conformalcoating registered
& tested UL 94 V0 ?
NO
YES
NO
FAR 25Flame Test
NO
YES
Flame Test Report
Design for a PWB
YES
PWB Laminates
registered & tested per IPC 4101 or
UL 94-V0?
*BOM = Bill Of Materials
Flammability Assured
BOM* Analysis Documented
IsPWB
registered & tested per UL 94- V0?
Page 18
Conclusions
• The FAA requires data for flammability certification of electronics before E/E components can be delivered on airplanes.
• Currently, all affected parts must be tested to 12-sec vertical for flammability certification
• Suppliers of E/E equipment need to put a priority on acquiring acceptable data far upstream of delivery.